{"created":"2023-06-20T15:03:05.599670+00:00","id":32202,"links":{},"metadata":{"_buckets":{"deposit":"ff475a39-57f3-480e-91f9-2d5dc735f668"},"_deposit":{"created_by":1,"id":"32202","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32202"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032202","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["407775","407779","407776","407777","407778","407780"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Adaptive time optimum control of an attitude control system using air jet"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1970-07","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"3_A","bibliographicPageEnd":"563","bibliographicPageStart":"549","bibliographicVolumeNumber":"6","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告では空気ジェットで一軸まわりの傾きを制御する系と,それの適応性をもった最適制御系について述べられている.純慣性系の最短詩問制御問題は,位相面上で放物線を組合わせた切換線を作り,最大操作トルクを用いればよいことが知られている.ここではバリスタという非線形抵抗素子を用いて切換線を実現している.最短時間制御をする制御系が働いている状態のまま,機体にはテストシグナルとして小さな振動が加えられて,軸まわりの慣性モーメントが相開法により測定される.その測定値により常に最適の切換線を自動的に設定することができる.モーメントを変化させて,確かに切換線が最適に設定されていることが実験的に確かめられた.慣性モーメントが変化したときの測定系の応答,およびテストシグナルの最短時間制御への影響や,測定誤差に及ぼす影響についての考察がなされている.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes the purely inertial system that can control its attitude on an axis by the air jet, and gives the results of the adaptive optimum control of the system. It is well known that the time optimum control of the purely inertial system can be accomplished by appling positive and negative maximum torque according to the parabolic switching curve in the phase plane. In order to realize the desired switching curve a nonlinear resistor-varistor-is used in this control system. Keeping the time optimum control loop closed, the small perturbation signal is applied to the system and the inertial moment of the controlled subject is measured by the correlation method. The result of the measurement of the moment is used in the adaptive control system to give the optimum switching curve in the phase plane automatically. By changing the moment, it is experimentally verified that the switching curve is optimally set. The response of the moment measuring system to the sudden change of the moment is described. Also the effects of the test signal on the time optimum control and error of the measured moment are stated.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125352000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"上野, 敏行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"五十嵐, 寿一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石井, 泰"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"UENO, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IGARASHI, Juichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHII, Yasushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA0125352.pdf","filesize":[{"value":"737.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125352.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32202/files/SA0125352.pdf"},"version_id":"b2105738-b402-46b7-bb2f-369a36e6b9e9"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"空気ジェットを用いた姿勢制御系の適応性をもった最短時間制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"空気ジェットを用いた姿勢制御系の適応性をもった最短時間制御"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32202","relation_version_is_last":true,"title":["空気ジェットを用いた姿勢制御系の適応性をもった最短時間制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:38:36.996910+00:00"}